Stability of leading-edge vortex pair on a slender delta wing

AIAA Journal

Volumn 34, Issue 6, 1996, Pages 1182-1187

  Huang, Ming Ke ^a,b,c   Chow, Chuen Yen ^a,b  

^a UNIVERSITY OF COLORADO   (United States)

^b Dept of Aerosp Eng Sciences ^*

^c NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

[No Author keywords available]

Indexed keywords

DELTA WING; INCOMPRESSIBLE FLOW; VORTEX FLOW; VORTEX PAIR;

EID: 0029672113     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13210     Document Type: Article

References (17)

1. Saffman, P. G., and Sheffield, J. S., "How over a Wing with an Attached Free Vortex," Studies in Applied Mathematics, Vol. 57, No. 2, 1977, pp. 107-117.
2. Rossow, V. J., "Lift Enhancement by an Externally Trapped Vortex," Journal of Aircraft, Vol. 15, No. 9, 1978, pp. 618-625.
3. Rossow, V. J., "Two-Fence Concept of Efficient Trapping of Vortices on Airfoils," Journal of Aircraft, Vol. 29, No. 5, 1992, pp. 847-855.
4. Rossow, V. J., "Aerodynamics of Airfoils with Vortex Trapped by Two Spanwise Fences," Journal of Aircraft, Vol. 31, No. 1, 1994, pp. 146-153.
5. Huang, M. K., and Chow, C. Y., "Trapping of a Free Vortex by Joukowski Airfoils," AIAA Journal, Vol. 20, No. 3, 1982, pp. 292-298.
6. Chow, C. Y, Huang, M. K., and Yan, C. Z., "Unsteady Flows About a Joukowski Airfoil in the Presence of Moving Vortices," AIAA Journal, Vol. 21, No. 5, 1985, pp. 657, 658.
7. Chow, C. Y, Chen, C. L., and Huang, M. K., "Trapping of a Free Vortex by Airfoils with Surface Suction," AIAA Journal, Vol. 24, No. 8, 1986, pp. 1217, 1218.
8. Riddle, T. W., Wadcock, A. J., Tso, J., and Cummings, R. M., "Experimental Analysis of Trapping Techniques," AIAA Paper 91-3271, Sept. 1991.
9. Lowson, M. V., "Some Experiments with Vortex Breakdown," Journal of the Aeronautical Society, Vol. 68, May 1964, pp. 343-346.
10. Nielson, J. N., Missile Aerodynamics, McGraw-Hill, New York, 1960.
11. Legendre, R., "Écoulement au Voisinage De La Pointe Avant D'une Aile A Forte Fléche Aux Incidences Moyennes," La Recherche Aeronautique, Bulletin Bimestriel, De L'Office National D'Études Et De Recherches Aéronautiques, Nov.-Dec. 1952 and Jan.-Feb. 1953.
12. Adams, M. C., "Leading-Edge Separation from Delta Wing at Supersonic Speeds," Journal of the Aeronautical Sciences, Vol. 20, No. 6, 1953, pp. 430, 431.
13. Brown, C. E., and Michael, W. H., Jr., "On Slender Wings with Leading Edge Separation," NACA TN 3430, April 1955.
14. Sychev, V. V, "Three-Dimensional Hypersonic Gas Flow Past Slender Bodies at High Angles of Attack," Journal of Mathematics and Mechanics (USSR), Vol. 24, Feb. 1960, pp. 296-306.
15. Pearson, C. E., Handbook of Applied Mathematics, Van Nostrand Reinold, New York, 1974, pp. 13, 14.
16. Hemsch, M. J., and Luckring, J. M., "Connection Between Leading-Edge Sweep, Vortex Lift and Vortex Strength for Delta Wings," Journal of Aircraft, Vol. 27 , No. 5, 1990, pp. 473-475.
17. Smith, J. H. B., "Calculations of the Flow over Thick, Conical, Slender Wings with Leading-Edge Separation," Aeronautical Research Council, ARC R&M 3694, London, March 1972.